mirror of https://github.com/ArduPilot/ardupilot
708 lines
24 KiB
Plaintext
708 lines
24 KiB
Plaintext
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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static void
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get_stabilize_roll(int32_t target_angle)
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{
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// angle error
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target_angle = wrap_180(target_angle - ahrs.roll_sensor);
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#if FRAME_CONFIG == HELI_FRAME
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// limit the error we're feeding to the PID
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target_angle = constrain(target_angle, -4500, 4500);
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// convert to desired Rate:
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target_angle = g.pi_stabilize_roll.get_pi(target_angle, G_Dt);
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// output control - we do not use rate controllers for helicopters so send directly to servos
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g.rc_1.servo_out = constrain(target_angle, -4500, 4500);
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#else
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// convert to desired Rate:
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int32_t target_rate = g.pi_stabilize_roll.get_p(target_angle);
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int16_t i_stab;
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if(labs(ahrs.roll_sensor) < 500) {
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target_angle = constrain(target_angle, -500, 500);
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i_stab = g.pi_stabilize_roll.get_i(target_angle, G_Dt);
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}else{
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i_stab = g.pi_stabilize_roll.get_integrator();
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}
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// set targets for rate controller
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set_roll_rate_target(target_rate+i_stab, EARTH_FRAME);
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#endif
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}
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static void
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get_stabilize_pitch(int32_t target_angle)
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{
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// angle error
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target_angle = wrap_180(target_angle - ahrs.pitch_sensor);
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#if FRAME_CONFIG == HELI_FRAME
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// limit the error we're feeding to the PID
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target_angle = constrain(target_angle, -4500, 4500);
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// convert to desired Rate:
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target_angle = g.pi_stabilize_pitch.get_pi(target_angle, G_Dt);
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// output control - we do not use rate controllers for helicopters so send directly to servos
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g.rc_2.servo_out = constrain(target_angle, -4500, 4500);
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#else
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// convert to desired Rate:
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int32_t target_rate = g.pi_stabilize_pitch.get_p(target_angle);
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int16_t i_stab;
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if(labs(ahrs.pitch_sensor) < 500) {
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target_angle = constrain(target_angle, -500, 500);
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i_stab = g.pi_stabilize_pitch.get_i(target_angle, G_Dt);
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}else{
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i_stab = g.pi_stabilize_pitch.get_integrator();
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}
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// set targets for rate controller
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set_pitch_rate_target(target_rate + i_stab, EARTH_FRAME);
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#endif
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}
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static void
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get_stabilize_yaw(int32_t target_angle)
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{
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int32_t target_rate,i_term;
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int32_t angle_error;
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int32_t output = 0;
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// angle error
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angle_error = wrap_180(target_angle - ahrs.yaw_sensor);
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// limit the error we're feeding to the PID
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#if FRAME_CONFIG == HELI_FRAME
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angle_error = constrain(angle_error, -4500, 4500);
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#else
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angle_error = constrain(angle_error, -4000, 4000);
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#endif
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// convert angle error to desired Rate:
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target_rate = g.pi_stabilize_yaw.get_p(angle_error);
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i_term = g.pi_stabilize_yaw.get_i(angle_error, G_Dt);
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// do not use rate controllers for helicotpers with external gyros
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#if FRAME_CONFIG == HELI_FRAME
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if(motors.ext_gyro_enabled) {
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g.rc_4.servo_out = constrain((target_rate + i_term), -4500, 4500);
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}
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#endif
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#if LOGGING_ENABLED == ENABLED
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static int8_t log_counter = 0; // used to slow down logging of PID values to dataflash
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// log output if PID logging is on and we are tuning the yaw
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if( g.log_bitmask & MASK_LOG_PID && (g.radio_tuning == CH6_YAW_KP || g.radio_tuning == CH6_YAW_RATE_KP) ) {
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log_counter++;
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if( log_counter >= 10 ) { // (update rate / desired output rate) = (100hz / 10hz) = 10
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log_counter = 0;
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Log_Write_PID(CH6_YAW_KP, angle_error, target_rate, i_term, 0, output, tuning_value);
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}
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}
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#endif
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// set targets for rate controller
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set_yaw_rate_target(target_rate+i_term, EARTH_FRAME);
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}
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static void
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get_acro_roll(int32_t target_rate)
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{
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target_rate = target_rate * g.acro_p;
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// set targets for rate controller
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set_roll_rate_target(target_rate, BODY_FRAME);
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}
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static void
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get_acro_pitch(int32_t target_rate)
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{
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target_rate = target_rate * g.acro_p;
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// set targets for rate controller
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set_pitch_rate_target(target_rate, BODY_FRAME);
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}
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static void
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get_acro_yaw(int32_t target_rate)
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{
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target_rate = target_rate * g.acro_p;
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// set targets for rate controller
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set_yaw_rate_target(target_rate, BODY_FRAME);
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}
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// Roll with rate input and stabilized in the earth frame
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static void
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get_roll_rate_stabilized_ef(int32_t stick_angle)
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{
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int32_t angle_error = 0;
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// convert the input to the desired roll rate
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int32_t target_rate = stick_angle * g.acro_p - (roll_axis * g.acro_balance_roll)/100;
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// convert the input to the desired roll rate
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roll_axis += target_rate * G_Dt;
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roll_axis = wrap_180(roll_axis);
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// ensure that we don't reach gimbal lock
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if (roll_axis > 4500 || roll_axis < -4500) {
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roll_axis = constrain(roll_axis, -4500, 4500);
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angle_error = wrap_180(roll_axis - ahrs.roll_sensor);
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} else {
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// angle error with maximum of +- max_angle_overshoot
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angle_error = wrap_180(roll_axis - ahrs.roll_sensor);
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angle_error = constrain(angle_error, -MAX_ROLL_OVERSHOOT, MAX_ROLL_OVERSHOOT);
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}
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if (motors.armed() == false || ((g.rc_3.control_in == 0) && !ap.failsafe)) {
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angle_error = 0;
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}
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// update roll_axis to be within max_angle_overshoot of our current heading
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roll_axis = wrap_180(angle_error + ahrs.roll_sensor);
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// set earth frame targets for rate controller
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// set earth frame targets for rate controller
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set_roll_rate_target(g.pi_stabilize_roll.get_p(angle_error) + target_rate, EARTH_FRAME);
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}
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// Pitch with rate input and stabilized in the earth frame
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static void
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get_pitch_rate_stabilized_ef(int32_t stick_angle)
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{
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int32_t angle_error = 0;
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// convert the input to the desired pitch rate
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int32_t target_rate = stick_angle * g.acro_p - (pitch_axis * g.acro_balance_pitch)/100;
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// convert the input to the desired pitch rate
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pitch_axis += target_rate * G_Dt;
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pitch_axis = wrap_180(pitch_axis);
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// ensure that we don't reach gimbal lock
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if (pitch_axis > 4500 || pitch_axis < -4500) {
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pitch_axis = constrain(pitch_axis, -4500, 4500);
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angle_error = wrap_180(pitch_axis - ahrs.pitch_sensor);
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} else {
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// angle error with maximum of +- max_angle_overshoot
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angle_error = wrap_180(pitch_axis - ahrs.pitch_sensor);
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angle_error = constrain(angle_error, -MAX_PITCH_OVERSHOOT, MAX_PITCH_OVERSHOOT);
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}
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if (motors.armed() == false || ((g.rc_3.control_in == 0) && !ap.failsafe)) {
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angle_error = 0;
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}
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// update pitch_axis to be within max_angle_overshoot of our current heading
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pitch_axis = wrap_180(angle_error + ahrs.pitch_sensor);
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// set earth frame targets for rate controller
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set_pitch_rate_target(g.pi_stabilize_pitch.get_p(angle_error) + target_rate, EARTH_FRAME);
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}
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// Yaw with rate input and stabilized in the earth frame
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static void
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get_yaw_rate_stabilized_ef(int32_t stick_angle)
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{
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int32_t angle_error = 0;
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// convert the input to the desired yaw rate
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int32_t target_rate = stick_angle * g.acro_p;
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// convert the input to the desired yaw rate
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nav_yaw += target_rate * G_Dt;
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nav_yaw = wrap_360(nav_yaw);
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// calculate difference between desired heading and current heading
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angle_error = wrap_180(nav_yaw - ahrs.yaw_sensor);
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// limit the maximum overshoot
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angle_error = constrain(angle_error, -MAX_YAW_OVERSHOOT, MAX_YAW_OVERSHOOT);
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if (motors.armed() == false || ((g.rc_3.control_in == 0) && !ap.failsafe)) {
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angle_error = 0;
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}
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// update nav_yaw to be within max_angle_overshoot of our current heading
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nav_yaw = wrap_360(angle_error + ahrs.yaw_sensor);
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// set earth frame targets for rate controller
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set_yaw_rate_target(g.pi_stabilize_yaw.get_p(angle_error)+target_rate, EARTH_FRAME);
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}
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// set_roll_rate_target - to be called by upper controllers to set roll rate targets in the earth frame
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void set_roll_rate_target( int32_t desired_rate, uint8_t earth_or_body_frame ) {
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rate_targets_frame = earth_or_body_frame;
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if( earth_or_body_frame == BODY_FRAME ) {
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roll_rate_target_bf = desired_rate;
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}else{
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roll_rate_target_ef = desired_rate;
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}
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}
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// set_pitch_rate_target - to be called by upper controllers to set pitch rate targets in the earth frame
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void set_pitch_rate_target( int32_t desired_rate, uint8_t earth_or_body_frame ) {
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rate_targets_frame = earth_or_body_frame;
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if( earth_or_body_frame == BODY_FRAME ) {
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pitch_rate_target_bf = desired_rate;
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}else{
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pitch_rate_target_ef = desired_rate;
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}
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}
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// set_yaw_rate_target - to be called by upper controllers to set yaw rate targets in the earth frame
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void set_yaw_rate_target( int32_t desired_rate, uint8_t earth_or_body_frame ) {
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rate_targets_frame = earth_or_body_frame;
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if( earth_or_body_frame == BODY_FRAME ) {
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yaw_rate_target_bf = desired_rate;
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}else{
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yaw_rate_target_ef = desired_rate;
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}
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}
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// update_rate_contoller_targets - converts earth frame rates to body frame rates for rate controllers
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void
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update_rate_contoller_targets()
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{
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if( rate_targets_frame == EARTH_FRAME ) {
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// convert earth frame rates to body frame rates
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roll_rate_target_bf = roll_rate_target_ef - sin_pitch * yaw_rate_target_ef;
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pitch_rate_target_bf = cos_roll_x * pitch_rate_target_ef + sin_roll * cos_pitch_x * yaw_rate_target_ef;
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yaw_rate_target_bf = cos_pitch_x * cos_roll_x * yaw_rate_target_ef - sin_roll * pitch_rate_target_ef;
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}
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}
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// run roll, pitch and yaw rate controllers and send output to motors
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// targets for these controllers comes from stabilize controllers
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void
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run_rate_controllers()
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{
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#if FRAME_CONFIG == HELI_FRAME // helicopters only use rate controllers for yaw and only when not using an external gyro
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if(!motors.ext_gyro_enabled) {
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g.rc_4.servo_out = get_rate_yaw(yaw_rate_target_bf);
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}
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#else
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// call rate controllers
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g.rc_1.servo_out = get_rate_roll(roll_rate_target_bf);
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g.rc_2.servo_out = get_rate_pitch(pitch_rate_target_bf);
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g.rc_4.servo_out = get_rate_yaw(yaw_rate_target_bf);
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#endif
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}
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static int16_t
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get_rate_roll(int32_t target_rate)
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{
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int32_t p,i,d; // used to capture pid values for logging
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int32_t current_rate; // this iteration's rate
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int32_t rate_error; // simply target_rate - current_rate
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int32_t output; // output from pid controller
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// get current rate
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current_rate = (omega.x * DEGX100);
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// call pid controller
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rate_error = target_rate - current_rate;
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p = g.pid_rate_roll.get_p(rate_error);
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// freeze I term if we've breached roll-pitch limits
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if( motors.reached_limit(AP_MOTOR_ROLLPITCH_LIMIT) ) {
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i = g.pid_rate_roll.get_integrator();
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}else{
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i = g.pid_rate_roll.get_i(rate_error, G_Dt);
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}
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d = g.pid_rate_roll.get_d(rate_error, G_Dt);
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output = p + i + d;
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// constrain output
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output = constrain(output, -5000, 5000);
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#if LOGGING_ENABLED == ENABLED
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static int8_t log_counter = 0; // used to slow down logging of PID values to dataflash
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// log output if PID logging is on and we are tuning the rate P, I or D gains
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if( g.log_bitmask & MASK_LOG_PID && (g.radio_tuning == CH6_RATE_KP || g.radio_tuning == CH6_RATE_KI || g.radio_tuning == CH6_RATE_KD) ) {
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log_counter++;
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if( log_counter >= 10 ) { // (update rate / desired output rate) = (100hz / 10hz) = 10
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log_counter = 0;
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Log_Write_PID(CH6_RATE_KP, rate_error, p, i, d /*-rate_d_dampener*/, output, tuning_value);
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}
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}
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#endif
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// output control
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return output;
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}
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static int16_t
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get_rate_pitch(int32_t target_rate)
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{
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int32_t p,i,d; // used to capture pid values for logging
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int32_t current_rate; // this iteration's rate
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int32_t rate_error; // simply target_rate - current_rate
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int32_t output; // output from pid controller
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// get current rate
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current_rate = (omega.y * DEGX100);
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// call pid controller
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rate_error = target_rate - current_rate;
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p = g.pid_rate_pitch.get_p(rate_error);
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// freeze I term if we've breached roll-pitch limits
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if( motors.reached_limit(AP_MOTOR_ROLLPITCH_LIMIT) ) {
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i = g.pid_rate_pitch.get_integrator();
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}else{
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i = g.pid_rate_pitch.get_i(rate_error, G_Dt);
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}
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d = g.pid_rate_pitch.get_d(rate_error, G_Dt);
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output = p + i + d;
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// constrain output
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output = constrain(output, -5000, 5000);
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#if LOGGING_ENABLED == ENABLED
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static int8_t log_counter = 0; // used to slow down logging of PID values to dataflash
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// log output if PID logging is on and we are tuning the rate P, I or D gains
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if( g.log_bitmask & MASK_LOG_PID && (g.radio_tuning == CH6_RATE_KP || g.radio_tuning == CH6_RATE_KI || g.radio_tuning == CH6_RATE_KD) ) {
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log_counter++;
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if( log_counter >= 10 ) { // (update rate / desired output rate) = (100hz / 10hz) = 10
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log_counter = 0;
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Log_Write_PID(CH6_RATE_KP+100, rate_error, p, i, d/*-rate_d_dampener*/, output, tuning_value);
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}
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}
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#endif
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// output control
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return output;
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}
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static int16_t
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get_rate_yaw(int32_t target_rate)
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{
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int32_t p,i,d; // used to capture pid values for logging
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int32_t rate_error;
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int32_t output;
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// rate control
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rate_error = target_rate - (omega.z * DEGX100);
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// separately calculate p, i, d values for logging
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p = g.pid_rate_yaw.get_p(rate_error);
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// freeze I term if we've breached yaw limits
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if( motors.reached_limit(AP_MOTOR_YAW_LIMIT) ) {
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i = g.pid_rate_yaw.get_integrator();
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}else{
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i = g.pid_rate_yaw.get_i(rate_error, G_Dt);
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}
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d = g.pid_rate_yaw.get_d(rate_error, G_Dt);
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output = p+i+d;
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output = constrain(output, -4500, 4500);
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#if LOGGING_ENABLED == ENABLED
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static int8_t log_counter = 0; // used to slow down logging of PID values to dataflash
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// log output if PID loggins is on and we are tuning the yaw
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if( g.log_bitmask & MASK_LOG_PID && (g.radio_tuning == CH6_YAW_KP || g.radio_tuning == CH6_YAW_RATE_KP) ) {
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log_counter++;
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if( log_counter >= 10 ) { // (update rate / desired output rate) = (100hz / 10hz) = 10
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log_counter = 0;
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Log_Write_PID(CH6_YAW_RATE_KP, rate_error, p, i, d, output, tuning_value);
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}
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}
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#endif
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#if FRAME_CONFIG == HELI_FRAME || FRAME_CONFIG == TRI_FRAME
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// constrain output
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return output;
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#else
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// output control:
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int16_t yaw_limit = 2200 + abs(g.rc_4.control_in);
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// smoother Yaw control:
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return constrain(output, -yaw_limit, yaw_limit);
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#endif
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}
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static int16_t
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get_throttle_rate(int16_t z_target_speed)
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{
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int32_t p,i,d; // used to capture pid values for logging
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int16_t z_rate_error, output = 0;
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// calculate rate error
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#if INERTIAL_NAV == ENABLED
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z_rate_error = z_target_speed - inertial_nav._velocity.z; // calc the speed error
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#else
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z_rate_error = z_target_speed - climb_rate; // calc the speed error
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#endif
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int16_t tmp = ((int32_t)z_target_speed * (int32_t)g.throttle_cruise) / 280;
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tmp = min(tmp, 500);
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// separately calculate p, i, d values for logging
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p = g.pid_throttle.get_p(z_rate_error);
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|
|
|
// freeze I term if we've breached throttle limits
|
|
if(motors.reached_limit(AP_MOTOR_THROTTLE_LIMIT)) {
|
|
i = g.pid_throttle.get_integrator();
|
|
}else{
|
|
i = g.pid_throttle.get_i(z_rate_error, .02);
|
|
}
|
|
d = g.pid_throttle.get_d(z_rate_error, .02);
|
|
|
|
//
|
|
// limit the rate
|
|
output += constrain(p+i+d, -150, 200);
|
|
|
|
#if LOGGING_ENABLED == ENABLED
|
|
static int8_t log_counter = 0; // used to slow down logging of PID values to dataflash
|
|
// log output if PID loggins is on and we are tuning the yaw
|
|
if( g.log_bitmask & MASK_LOG_PID && g.radio_tuning == CH6_THROTTLE_KP ) {
|
|
log_counter++;
|
|
if( log_counter >= 10 ) { // (update rate / desired output rate) = (50hz / 10hz) = 5hz
|
|
log_counter = 0;
|
|
Log_Write_PID(CH6_THROTTLE_KP, z_rate_error, p, i, d, output, tuning_value);
|
|
}
|
|
}
|
|
#endif
|
|
|
|
return output;
|
|
}
|
|
|
|
// Keeps old data out of our calculation / logs
|
|
static void reset_nav_params(void)
|
|
{
|
|
nav_throttle = 0;
|
|
|
|
// always start Circle mode at same angle
|
|
circle_angle = 0;
|
|
|
|
// We must be heading to a new WP, so XTrack must be 0
|
|
crosstrack_error = 0;
|
|
|
|
// Will be set by new command
|
|
target_bearing = 0;
|
|
|
|
// Will be set by new command
|
|
wp_distance = 0;
|
|
|
|
// Will be set by new command, used by loiter
|
|
long_error = 0;
|
|
lat_error = 0;
|
|
nav_lon = 0;
|
|
nav_lat = 0;
|
|
nav_roll = 0;
|
|
nav_pitch = 0;
|
|
auto_roll = 0;
|
|
auto_pitch = 0;
|
|
|
|
// make sure we stick to Nav yaw on takeoff
|
|
auto_yaw = nav_yaw;
|
|
}
|
|
|
|
/*
|
|
* reset all I integrators
|
|
*/
|
|
static void reset_I_all(void)
|
|
{
|
|
reset_rate_I();
|
|
reset_stability_I();
|
|
reset_wind_I();
|
|
reset_throttle_I();
|
|
reset_optflow_I();
|
|
|
|
// This is the only place we reset Yaw
|
|
g.pi_stabilize_yaw.reset_I();
|
|
}
|
|
|
|
static void reset_rate_I()
|
|
{
|
|
g.pid_rate_roll.reset_I();
|
|
g.pid_rate_pitch.reset_I();
|
|
g.pid_rate_yaw.reset_I();
|
|
}
|
|
|
|
static void reset_optflow_I(void)
|
|
{
|
|
g.pid_optflow_roll.reset_I();
|
|
g.pid_optflow_pitch.reset_I();
|
|
of_roll = 0;
|
|
of_pitch = 0;
|
|
}
|
|
|
|
static void reset_wind_I(void)
|
|
{
|
|
// Wind Compensation
|
|
// this i is not currently being used, but we reset it anyway
|
|
// because someone may modify it and not realize it, causing a bug
|
|
g.pi_loiter_lat.reset_I();
|
|
g.pi_loiter_lon.reset_I();
|
|
|
|
g.pid_loiter_rate_lat.reset_I();
|
|
g.pid_loiter_rate_lon.reset_I();
|
|
|
|
g.pid_nav_lat.reset_I();
|
|
g.pid_nav_lon.reset_I();
|
|
}
|
|
|
|
static void reset_throttle_I(void)
|
|
{
|
|
// For Altitude Hold
|
|
g.pi_alt_hold.reset_I();
|
|
g.pid_throttle.reset_I();
|
|
}
|
|
|
|
static void reset_stability_I(void)
|
|
{
|
|
// Used to balance a quad
|
|
// This only needs to be reset during Auto-leveling in flight
|
|
g.pi_stabilize_roll.reset_I();
|
|
g.pi_stabilize_pitch.reset_I();
|
|
}
|
|
|
|
|
|
/*************************************************************
|
|
* throttle control
|
|
****************************************************************/
|
|
|
|
static int16_t get_angle_boost(int16_t value)
|
|
{
|
|
float temp = cos_pitch_x * cos_roll_x;
|
|
temp = constrain(temp, .75, 1.0);
|
|
return ((float)(value + 80) / temp) - (value + 80);
|
|
}
|
|
|
|
#if FRAME_CONFIG == HELI_FRAME
|
|
// heli_angle_boost - adds a boost depending on roll/pitch values
|
|
// equivalent of quad's angle_boost function
|
|
// throttle value should be 0 ~ 1000
|
|
static int16_t heli_get_angle_boost(int16_t throttle)
|
|
{
|
|
float angle_boost_factor = cos_pitch_x * cos_roll_x;
|
|
angle_boost_factor = 1.0 - constrain(angle_boost_factor, .5, 1.0);
|
|
int16_t throttle_above_mid = max(throttle - motors.throttle_mid,0);
|
|
return throttle + throttle_above_mid*angle_boost_factor;
|
|
|
|
}
|
|
#endif // HELI_FRAME
|
|
|
|
// calculate modified roll/pitch depending upon optical flow calculated position
|
|
static int32_t
|
|
get_of_roll(int32_t input_roll)
|
|
{
|
|
#if OPTFLOW == ENABLED
|
|
static float tot_x_cm = 0; // total distance from target
|
|
static uint32_t last_of_roll_update = 0;
|
|
int32_t new_roll = 0;
|
|
int32_t p,i,d;
|
|
|
|
// check if new optflow data available
|
|
if( optflow.last_update != last_of_roll_update) {
|
|
last_of_roll_update = optflow.last_update;
|
|
|
|
// add new distance moved
|
|
tot_x_cm += optflow.x_cm;
|
|
|
|
// only stop roll if caller isn't modifying roll
|
|
if( input_roll == 0 && current_loc.alt < 1500) {
|
|
p = g.pid_optflow_roll.get_p(-tot_x_cm);
|
|
i = g.pid_optflow_roll.get_i(-tot_x_cm,1.0); // we could use the last update time to calculate the time change
|
|
d = g.pid_optflow_roll.get_d(-tot_x_cm,1.0);
|
|
new_roll = p+i+d;
|
|
}else{
|
|
g.pid_optflow_roll.reset_I();
|
|
tot_x_cm = 0;
|
|
p = 0; // for logging
|
|
i = 0;
|
|
d = 0;
|
|
}
|
|
// limit amount of change and maximum angle
|
|
of_roll = constrain(new_roll, (of_roll-20), (of_roll+20));
|
|
|
|
#if LOGGING_ENABLED == ENABLED
|
|
static int8_t log_counter = 0; // used to slow down logging of PID values to dataflash
|
|
// log output if PID logging is on and we are tuning the rate P, I or D gains
|
|
if( g.log_bitmask & MASK_LOG_PID && (g.radio_tuning == CH6_OPTFLOW_KP || g.radio_tuning == CH6_OPTFLOW_KI || g.radio_tuning == CH6_OPTFLOW_KD) ) {
|
|
log_counter++;
|
|
if( log_counter >= 5 ) { // (update rate / desired output rate) = (100hz / 10hz) = 10
|
|
log_counter = 0;
|
|
Log_Write_PID(CH6_OPTFLOW_KP, tot_x_cm, p, i, d, of_roll, tuning_value);
|
|
}
|
|
}
|
|
#endif // LOGGING_ENABLED == ENABLED
|
|
}
|
|
|
|
// limit max angle
|
|
of_roll = constrain(of_roll, -1000, 1000);
|
|
|
|
return input_roll+of_roll;
|
|
#else
|
|
return input_roll;
|
|
#endif // OPTFLOW == ENABLED
|
|
}
|
|
|
|
static int32_t
|
|
get_of_pitch(int32_t input_pitch)
|
|
{
|
|
#if OPTFLOW == ENABLED
|
|
static float tot_y_cm = 0; // total distance from target
|
|
static uint32_t last_of_pitch_update = 0;
|
|
int32_t new_pitch = 0;
|
|
int32_t p,i,d;
|
|
|
|
// check if new optflow data available
|
|
if( optflow.last_update != last_of_pitch_update ) {
|
|
last_of_pitch_update = optflow.last_update;
|
|
|
|
// add new distance moved
|
|
tot_y_cm += optflow.y_cm;
|
|
|
|
// only stop roll if caller isn't modifying pitch
|
|
if( input_pitch == 0 && current_loc.alt < 1500 ) {
|
|
p = g.pid_optflow_pitch.get_p(tot_y_cm);
|
|
i = g.pid_optflow_pitch.get_i(tot_y_cm, 1.0); // we could use the last update time to calculate the time change
|
|
d = g.pid_optflow_pitch.get_d(tot_y_cm, 1.0);
|
|
new_pitch = p + i + d;
|
|
}else{
|
|
tot_y_cm = 0;
|
|
g.pid_optflow_pitch.reset_I();
|
|
p = 0; // for logging
|
|
i = 0;
|
|
d = 0;
|
|
}
|
|
|
|
// limit amount of change
|
|
of_pitch = constrain(new_pitch, (of_pitch-20), (of_pitch+20));
|
|
|
|
#if LOGGING_ENABLED == ENABLED
|
|
static int8_t log_counter = 0; // used to slow down logging of PID values to dataflash
|
|
// log output if PID logging is on and we are tuning the rate P, I or D gains
|
|
if( g.log_bitmask & MASK_LOG_PID && (g.radio_tuning == CH6_OPTFLOW_KP || g.radio_tuning == CH6_OPTFLOW_KI || g.radio_tuning == CH6_OPTFLOW_KD) ) {
|
|
log_counter++;
|
|
if( log_counter >= 5 ) { // (update rate / desired output rate) = (100hz / 10hz) = 10
|
|
log_counter = 0;
|
|
Log_Write_PID(CH6_OPTFLOW_KP+100, tot_y_cm, p, i, d, of_pitch, tuning_value);
|
|
}
|
|
}
|
|
#endif // LOGGING_ENABLED == ENABLED
|
|
}
|
|
|
|
// limit max angle
|
|
of_pitch = constrain(of_pitch, -1000, 1000);
|
|
|
|
return input_pitch+of_pitch;
|
|
#else
|
|
return input_pitch;
|
|
#endif // OPTFLOW == ENABLED
|
|
}
|